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Oil-electric hybrid unmanned aerial vehicle tripod-head assembly

A kind of technology of mobile platform and drone, which is applied in the field of oil-electric hybrid drone platform components, which can solve the problems of poor shock absorption effect and unreasonable structural design, etc., and achieve compact structure, stable shooting and extended distance Effect

Pending Publication Date: 2018-11-13
GUANGZHOU WALKERA TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to provide a hybrid unmanned aerial vehicle platform assembly to solve the problems of unreasonable structure design and poor shock absorption effect of the hybrid unmanned aerial vehicle platform in the prior art

Method used

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  • Oil-electric hybrid unmanned aerial vehicle tripod-head assembly
  • Oil-electric hybrid unmanned aerial vehicle tripod-head assembly
  • Oil-electric hybrid unmanned aerial vehicle tripod-head assembly

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Embodiment Construction

[0053] The present application will be further described below in combination with specific embodiments. Wherein, the same or similar symbols in the accompanying drawings of the embodiments of the present application correspond to the same or similar components, which are only used for exemplary illustrations and cannot be understood as limitations on the present application; in order to better illustrate the embodiments of the present application, a certain Some parts will be omitted, enlarged or reduced, and do not represent the size of the actual product; the orientation or positional relationship indicated by the terms "upper", "lower", "left", "right" in the embodiments of this application are based on the accompanying drawings The orientation or positional relationship shown, rather than indicating or implying that the device or element referred to must have a specific orientation or be constructed in a specific orientation. For those of ordinary skill in the art, the spe...

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Abstract

The invention relates to an oil-electric hybrid unmanned aerial vehicle tripod-head assembly which comprises a fuselage and a plurality of rotor wings evenly arranged on the side face of the fuselageat intervals; an engine, a generator and a tripod-head assembly body are arranged at the bottom of the fuselage; an oil tank is arranged at the top end of the fuselage; a control system is arranged inthe fuselage; the tripod-head assembly body comprises a camera and a damping device; the damping device comprises a U-shaped bracket, a Z-shaped bracket and a buffer bracket which are sequentially connected; the two sides of the U-shaped bracket are connected with the camera, one side of the U-shaped bracket is provided with a motor capable of controlling the camera to rotate up and down, and themotor is electrically connected with the control system; the buffer bracket comprises an upper bottom face and a lower bottom face; one end of the Z-shaped bracket is connected with the U-shaped bracket, and the other end of the Z-shaped bracket is connected with the lower bottom face of the buffer bracket; and the upper bottom face of the buffer bracket is connected with the fuselage.

Description

technical field [0001] The invention belongs to the technical field of oil-electric hybrid unmanned aerial vehicles, and in particular relates to a pan-tilt assembly of an oil-electric hybrid unmanned aerial vehicle. Background technique [0002] With the development of high-tech, unmanned aerial vehicle technology continues to make breakthroughs, unmanned aerial vehicle will be developed rapidly and more widely used. In the field of drones, although a series of advanced technologies such as visual positioning, high-definition image transmission, and sensory barriers continue to develop, the fundamental problem of battery life has not been effectively resolved. [0003] The multi-rotor UAV relies on the lift generated by multiple rotors to balance the gravity of the aircraft, so that the aircraft can fly, and the stability and attitude of the aircraft can be controlled by changing the speed of each rotor. Therefore, the multi-rotor aircraft can hover and fly at any speed wi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/08B64D27/02
CPCB64D27/02B64D47/08B64U50/11B64U50/19B64U2101/30B64U10/10B64D27/026
Inventor 罗之洪李奔夏烨罗强
Owner GUANGZHOU WALKERA TECH CO LTD